固体推进剂燃速测试技术研究进展  

Research Progress in the Burning Rate Measurement Technology of Solid Propellant

作　　者：裴庆[1] 赵凤起[1] 罗阳[1] 徐司雨[1] 

机构地区：[1]西安近代化学研究所燃烧与爆炸技术重点实验室,陕西西安710065

出　　处：《火炸药学报》2015年第3期9-14,21,共7页Chinese Journal of Explosives & Propellants

基　　金：国家自然科学基金资助(No.21473130)

摘　　要：综述了固体推进剂的静态燃速、动态燃速和特定环境下的燃烧测试技术的研究现状以及各种燃速测试方法的特点,分析认为固体推进剂燃速测试技术的总体发展规律是由静态燃速测试逐步发展到动态燃速测试,在动态燃速测试的基础上出现了旋转过载燃速测试技术和压强瞬变条件下的燃速测试技术。现有燃速测试技术还用于测试固体推进剂常用高能添加剂的燃烧性能。提出了固体推进剂燃烧性能测试技术的发展方向:高压(超高压)燃烧性能测试技术、超低压(真空)燃烧性能测试技术、低温微重力环境下的燃烧性能测试技术等。附参考文献55篇。The current research situation of static burning rate,dynamic burning rate and measurement technology of burning rate under specific environment for solid propellant,and characteristics of various burning rate measure-ment methods were reviewed.Considering that the general development rule of solid propellant burning rate meas-urement technology is that from the static burning rate measurement gradually developed into the dynamic burning rate measurement.On the basis of the dynamic burning rate measurement,the rotating overload burning rate meas-urement technology and burning rate measurement technology under the transient pressure condition appeared.The existing burning rate measurement technology is also used to test the combustion performance of commonly used high-energy additives in solid propellant.The future development direction of the combustion performance testing technology of solid propellant,including high pressure （ultra pressure）combustion performance measurement tech-nology,ultra low pressure （vacuum,）combustion performance measurement technology and low temperature micro-gravity combustion performance measurement technology etc,is pointed out with 55 references.

关 键 词：物理化学 固体推进剂 静态燃速 动态燃速 燃速测试 

分 类 号：TJ55[兵器科学与技术—军事化学与烟火技术] V512[航空宇航科学与技术—航空宇航推进理论与工程]